Effect Of Trailing Edge Geometry And Thickness On The Performance Of Certain Turbine Stator Blading

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Effect Of Trailing Edge Geometry And Thickness On The Performance Of Certain Turbine Stator Blading

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Author : Herman W. Prust
language : en
Publisher:
Release Date : 1972

Effect Of Trailing Edge Geometry And Thickness On The Performance Of Certain Turbine Stator Blading written by Herman W. Prust and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Fluid dynamics categories.

The experimental and analytical investigation included solid blades with five different trailing-edge thicknesses and four different trailing-edge geometries. One of the geometries was round, one was square, one was tapered from the suction surface, and the other tapered from the pressure surface. One of the trailing-edge thicknesses was sharp edged; the other four thicknesses were equivalent to about 5, 11, 16, and 20 percent of the blade throat width. The experimental results show increased efficiency loss for increased trailing-edge thickness for all trailing-edge geometries. The blade with round trailing edge, equal to about 11 percent of the blade throat width, had 60 percent more loss than the sharp-edged blade. For the same trailing-edge thickness, square trailing edges caused more loss than round trailing edges, and the tapered trailing edges caused about the same loss as the round trailing edges.

Effect Of Trailing Edge Geometry And Thickness On The Performance Of Certain Turbine Stator Blading

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Author : Herman W. Prust
language : en
Publisher:
Release Date : 1972

Effect Of Trailing Edge Geometry And Thickness On The Performance Of Certain Turbine Stator Blading written by Herman W. Prust and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.

Effect Of Trailing Edge Geometry And Thickness On The Performance Of Certain Turbine Stator Blading

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Author : Herman W. Prust (jr.)
language : en
Publisher:
Release Date : 1972

Effect Of Trailing Edge Geometry And Thickness On The Performance Of Certain Turbine Stator Blading written by Herman W. Prust (jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1972

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1991

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with Aeronautics categories.

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Monthly Catalog Of United States Government Publications

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Author :
language : en
Publisher:
Release Date : 1975-09

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975-09 with Government publications categories.

Gas Turbine Blade Cooling

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Author : Chaitanya D Ghodke
language : en
Publisher: SAE International
Release Date : 2018-12-10

Gas Turbine Blade Cooling written by Chaitanya D Ghodke and has been published by SAE International this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-12-10 with Technology & Engineering categories.

Gas turbines play an extremely important role in fulfilling a variety of power needs and are mainly used for power generation and propulsion applications. The performance and efficiency of gas turbine engines are to a large extent dependent on turbine rotor inlet temperatures: typically, the hotter the better. In gas turbines, the combustion temperature and the fuel efficiency are limited by the heat transfer properties of the turbine blades. However, in pushing the limits of hot gas temperatures while preventing the melting of blade components in high-pressure turbines, the use of effective cooling technologies is critical. Increasing the turbine inlet temperature also increases heat transferred to the turbine blade, and it is possible that the operating temperature could reach far above permissible metal temperature. In such cases, insufficient cooling of turbine blades results in excessive thermal stress on the blades causing premature blade failure. This may bring hazards to the engine's safe operation. Gas Turbine Blade Cooling, edited by Dr. Chaitanya D. Ghodke, offers 10 handpicked SAE International's technical papers, which identify key aspects of turbine blade cooling and help readers understand how this process can improve the performance of turbine hardware.

Monthly Catalog Of United States Government Publications

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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1966

Monthly Catalog Of United States Government Publications written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Government publications categories.

Monthly Catalog Of United States Government Publications Cumulative Index

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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1976

Monthly Catalog Of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with United States categories.

Nasa Technical Memorandum

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Author :
language : en
Publisher:
Release Date : 1975

Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aeronautics categories.